CROSS REFERENCE TO RELATED APPLICATIONS
[0001] This represents the first application directed towards the subject-matter.
FIELD
[0002] This disclosure relates to a scanning apparatus, and in particular, to a method for
scanning a plurality of components of similar design.
BACKGROUND
[0003] X-ray scans such as computed tomography (CT) scans are conventionally used in industry
for detecting defects such as voids, cracks, and inclusions, based on differences
in X-ray absorption in these regions. CT techniques can also be used for investigative
work on subjects such as aerofoil blades, and in particular, turbine blades of gas
turbine engines. In particular, CT may be used to produce three-dimensional (3D) representations
of a component. Generally, during a CT scan, x-ray beams that are generated by an
x-ray source penetrate the subject to be scanned. The x-ray beam, after being attenuated
by different densities of material within the subject, impinges upon an array of radiation
detectors. The array of radiation detectors produces electrical signals indicative
of the attenuated x-ray beam, thereby generating an x-ray image.
[0004] To produce a 3D model, 2D images of the component are taken from multiple angles
and the images are computationally combined. 3D CT is an emerging technology for the
inspection of dense metal parts such as those produced by additive manufacturing that
can have non-line of sight surfaces and cannot be inspected by other methods. A 3DCT
scan typically involves rotating the component about an axis, either through a full
360-degree rotation or a partial rotation. The axis of rotation can lie in a flat
plane, be inclined, or follow a more complex 3D trajectory. During scanning, part
of the x-rays is attenuated by a material of the component, some are scattered, and
the remaining are transmitted through the component to fall on the detector. 2D x-ray
images are significantly affected by scatter. Original equipment manufacturers (OEMs)
have therefore developed technologies, e.g. hardware and software, to correct scatter
and thereby reduce errors.
[0005] In addition to 3D CT, 2D CT is another form of CT where the detector is a linear
detector rather than a 2D detector. 2D CT can only create a thin cross-section image
of the part compared to 3D CT which generated the full volumetric data. However, 2D
CT has the advantage of being less affected by scatter. However, 3D CT is more sensitive
to scatter, particularly when scanning multiple dense objects, which can significantly
degrade image quality. Conventional scatter correction solution often requires a reference
scan that is free of scatter. These reference scans quantify scatter in each x-ray
projections and facilitate removal of the scatter during image reconstruction. Traditional
scatter correction methods involve creating a reference image for each X-ray projection.
This reference image is created using a variety of methods that range from scatter
free 2DCT scans stacked to form a 3D volume, to scatter correct grids or scatter reduction
arrays or even simulations. However, the creation of the reference image from the
stack of 2DCT scans is time consuming. Accordingly, in case of multi-part scanning,
the scanning time to create reference images is significantly increased, which is
not desired.
SUMMARY
[0006] According to a first aspect, a method for scanning a plurality of components of similar
design is provided. The method includes providing an imaging beam source, an imaging
beam receiver, and a support platform. The imaging beam source and the imaging beam
receiver are oppositely disposed to either side of the support platform. The method
further includes disposing the plurality of components on the support platform such
that the plurality of components is positioned axi-symmetrically and spaced apart
from each other by a first angular range. The method further includes generating,
by the imaging beam source, an imaging beam that passes through the plurality of components.
The method further includes collecting a first projection of at least one component
of the plurality of components at the imaging beam receiver. The first projection
includes a combination of a primary image of the at least one component and a scatter
image of the at least one component. The primary image includes a scatter free projection
of the at least one component. The method further includes collecting a second projection
of the at least one component at the imaging beam receiver. The second projection
includes the primary image of the at least one component. The method further includes
comparing, by a processor, the first projection and the second projection. The method
further includes generating, by the processor, the scatter image based on the comparison
of the first projection and the second projection. The method further includes storing,
by the processor, the scatter image of the at least one component in a memory. The
method further includes rotating and/or revolving the support platform by a second
angular range relative to the imaging beam source and the imaging beam receiver about
one or more axes. The second angular range is equal to the first angular range or
greater than the first angular range by at most 20 degrees. The method further includes
collecting, at different relative angles of rotation and/or revolution of the support
platform by the second angular range, further projections of the plurality of components
at the imaging beam receiver. The method further includes comparing, by the processor,
the further projections and the scatter image. The method further includes generating,
by the processor, further primary images of the plurality of components based on the
comparison of the further projections and the scatter image. The further primary images
include corresponding further scatter free projections of the plurality of components.
[0007] With axi-symmetric arrangement of the plurality of components of similar design on
the support platform, and with each component spaced apart by a predetermined angular
range (i.e., the first angular range), the method of the present disclosure may eliminate
a need for a full 360-degrees rotation for collecting projections of various components.
This arrangement of the plurality of components of similar design may ensure periodic
repetition of projections at different relative angles of rotation and/or revolution
of the support platform by the second angular range. Such periodic repetition of the
projections may enable the method of the present disclosure to perform scatter correction
only once. This may significantly reduce scanning time and computational efforts required
to generate the reference scatter image, which was otherwise needed to be generated
for each projection in conventional scanning methods. Therefore, the method of the
present disclosure may improve efficiency and accuracy of the scanning process for
investigating the plurality of components of similar design. Accordingly, the method
of the present disclosure may enable the simultaneous and effective scanning of the
plurality of components of similar design, which may further reduce operational cost
involved with the scanning.
[0008] It should be noted that "components of similar design" refers to components that
have similar shape, or components that are axi-symmetric (i.e., symmetrical around
one axis). For examples, components, such as gears will be considered as components
of similar design.
[0009] In some embodiments, comparing the first projection and the second projection includes
subtracting the second projection from the first projection. Further, the method includes
generating the scatter image based on subtraction of the second projection from the
first projection. In other applications, the first projection may be subtracted from
the second projection. By subtracting the second projection from the first projection
(or the first projection from the second projection), a reference scatter image is
generated, which may be used for scatter correction for further projections at different
relative angles of rotation and/or revolution of the support platform by the second
angular range.
[0010] In some embodiments, comparing the further projections and the scatter image includes
subtracting the scatter image from each of the further projections. Further, the method
includes generating the further primary images of the plurality of components based
on subtraction of the scatter image from each of the corresponding further projections.
The reference scatter image is then subtracted from the further projections of the
plurality of components. Accordingly, a high-quality primary image is obtained in
each of the further projections while minimizing an impact of scatter.
[0011] In some embodiments, the first angular range is at least 5 degrees, at least 10 degrees,
at least 20 degrees, at least 30 degrees, at least 45 degrees, at least 60 degrees,
at least 90 degrees, at least 120 degrees, at least 135 degrees, at least 150 degrees,
at least 170 degrees, at least 200 degrees, at least 230 degrees, or at least 270
degrees.
[0012] In some embodiments, the second angular range is at least 5 degrees, at least 10
degrees, at least 15 degrees, at least 25 degrees, at least 35 degrees, at least 50
degrees, at least 65 degrees, at least 95 degrees, at least 125 degrees, at least
140 degrees, at least 155 degrees, at least 175 degrees, at least 200 degrees, at
least 230 degrees, at least 270 degrees, or at least 290 degrees.
[0013] In some embodiments, the plurality of components is positioned axi-symmetrically
in a two-dimensional geometrical figure, such as a circle, a triangle, an ellipse,
a rectangle, a square, or a polygon. For example, the plurality of components is positioned
on vertices of a triangle. For example, the plurality of components is positioned
on vertices of a square.
[0014] In some embodiments, the plurality of components is positioned axi-symmetrically
in a three-dimensional geometrical figure, such as an ellipsoid, a sphere, a cube,
a cuboid, a prism, or a cylinder. This arrangement of the plurality of components
in the three-dimensional geometrical figure may ensure proper utilization of available
space to accommodate the plurality of components on the support platform. For example,
the plurality of components is positioned on corners of a cube.
[0015] In some embodiments, the plurality of components is positioned axi-symmetrically
in two or more concentric geometrical figures. This may ensure proper utilization
of available space to accommodate the plurality of components on the support platform.
[0016] In some embodiments, the two or more concentric geometrical figures have same shapes.
For example, some of the components may be positioned axi-symmetrically in a first
circle and rest of the components may be positioned axi-symmetrically in a second
circle that is concentric with the first circle.
[0017] In some embodiments, the two or more concentric geometrical figures have different
shapes. For example, some of the components may be positioned axi-symmetrically in
a circle and rest of the components may be positioned axi-symmetrically in a square
that is concentric with the circle.
[0018] In some embodiments, the method further includes maintaining substantially similar
imaging parameters while collecting the further projections. By maintaining substantially
similar imaging parameters, a consistent image quality may be obtained for all further
projections of the plurality of components. Imaging parameters may include a distance
between different components of a scanning apparatus, a voltage of the imaging beam
source, and so on.
[0019] In some embodiments, the plurality of components is positioned offset from the one
or more axes of rotation and/or revolution. This means that centres of the plurality
of components are displaced from the one or more axes of rotation and/or revolution.
This may improve image quality and contrast of the scan. This may also reduce the
concave wall effect.
[0020] In some embodiments, the method further includes selectively disposing an anti-scatter
unit either between the support platform and the imaging beam receiver or between
the support platform and the imaging beam source. Placement of the anti-scatter unit
either between the support platform and the imaging beam receiver or between the support
platform and the imaging beam source may eliminate scattered radiation, thereby improving
clarity and accuracy of the image. The anti-scatter unit is mainly used to obtain
a scatter free image of an object.
[0021] In some embodiments, collecting the second projection of the at least one component
at the imaging beam receiver further includes collecting the second projection of
the at least one component at the imaging beam receiver while the anti-scatter unit
is disposed between the support platform and the imaging beam receiver, or between
the support platform and the imaging beam source. By placing the anti-scatter unit
between the support platform and the imaging beam receiver, or between the support
platform and the imaging beam source, the scattered radiation may be filtered. Accordingly,
the reference scatter image (the second projection) may be generated, which may be
used for scatter correction in the further projections.
[0022] In some embodiments, the anti-scatter unit includes an anti-scatter grid, a beam
stopper, a hole plate array, or a collimation grid. The anti-scatter grid is often
used in CT scanning to reduce the scattered radiation generated from an object to
be scanned. The hole plate array may block the imaging beam from deviating from a
primary beam path, thereby capturing scatter free projections at the imaging beam
receiver.
[0023] According to a second aspect, a scanning apparatus for scanning a plurality of components
of similar design is provided. The scanning apparatus includes an imaging beam source
configured to generate an imaging beam that passes through the plurality of components.
The scanning apparatus further includes an imaging beam receiver configured to receive
the imaging beam, such that the plurality of components is disposed between the imaging
beam source and the imaging beam receiver. The scanning apparatus further includes
an anti-scatter unit. The scanning apparatus further includes a support platform configured
to support the plurality of components. The support platform is configured to rotate
and/or revolve relative to the imaging beam source and the imaging beam receiver about
one or more axes. The support platform is disposed between the imaging beam source
and the imaging beam receiver. The plurality of components is positioned axi-symmetrically
and spaced apart from each other by a first angular range. The scanning apparatus
further includes a processor communicably coupled to the imaging beam receiver and
configured to collect, in absence of the anti-scatter unit, a first projection of
at least one component of the plurality of components at the imaging beam receiver.
The first projection includes a combination of a primary image of the at least one
component and a scatter image of the at least one component. The primary image includes
a scatter free projection of the at least one component. The processor is further
configured to collect, in presence of the anti-scatter unit, a second projection of
the at least one component at the imaging beam receiver. The second projection includes
the primary image of the at least one component. The processor is further configured
to compare the first projection and the second projection. The processor is further
configured to generate the scatter image based on the comparison of the first projection
and the second projection. The processor is further configured to store the scatter
image of the at least one component in a memory. The processor is further configured
to collect, at different relative angles of rotation and/or revolution of the support
platform and in absence of the anti-scatter unit, further projections of the plurality
of components at the imaging beam receiver. The support platform is configured to
rotate and/or revolve by a second angular range relative to the imaging beam source
and the imaging beam receiver about one or more axes. The second angular range is
equal to or greater than the first angular range by at most 20 degrees. The processor
is further configured to compare the further projections and the scatter image. The
processor is further configured to generate further primary images of the plurality
of components based on the comparison of the further projections and the scatter image.
The further primary images include corresponding further scatter free projections
of the plurality of components.
[0024] With axi-symmetric arrangement of the plurality of components of similar design on
the support platform, and with each component spaced apart by a predetermined angular
range (i.e., the first angular range), the scanning apparatus of the present disclosure
may eliminate a need for a full 360-degrees rotation for collecting projections of
various components. This arrangement of the plurality of components of similar design
may ensure periodic repetition of projections at different relative angles of rotation
and/or revolution of the support platform by the second angular range. Such periodic
repetition of the projections may enable the scanning apparatus of the present disclosure
to perform scatter correction only once. Accordingly, the scanning apparatus of the
present disclosure may enable the simultaneous and effective scanning of the plurality
of components, which may further reduce operational cost involved with the scanning.
[0025] In some embodiments, the processor is further configured to compare the first projection
and the second projection by subtracting the second projection from the first projection.
The processor is further configured to generate the scatter image by subtracting the
second projection from the first projection. In other applications, the first projection
may be subtracted from the second projection. By subtracting the second projection
from the first projection (or the first projection from the second projection), a
reference scatter image is generated, which may be used for scatter correction for
further projections at different relative angles of rotation and/or revolution of
the support platform by the second angular range. Moreover, the scatter image is saved
in the memory of the processor.
[0026] In some embodiments, the processor is further configured to compare the further projections
and the scatter image by subtracting the scatter image from each of the further projections.
The processor is further configured to generate the further primary images of the
plurality of components by subtracting the scatter image from each of the corresponding
further projections. Accordingly, a high-quality image is obtained while minimizing
an impact of scatter.
[0027] In some embodiments, the plurality of components is positioned offset from the one
or more axes of rotation and/or revolution. This may improve image quality and contrast
of the scan. This may also reduce the concave wall effect.
[0028] In some embodiments, the anti-scatter unit is selectively disposed either between
the support platform and the imaging beam receiver, or between the support platform
and the imaging beam source. Placement of the anti-scatter unit either between the
support platform and the imaging beam receiver or between the support platform and
the imaging beam source may eliminate scattered radiation, thereby improving clarity
and accuracy of the image.
[0029] In some embodiments, the anti-scatter unit includes an anti-scatter grid, a beam
stopper, a hole plate array, or a collimation grid.
BRIEF DESCRIPTION OF THE DRAWINGS
[0030] Embodiments will now be described by way of example only with reference to the accompanying
drawings, in which:
FIG. 1 shows a schematic sectional side view of a gas turbine engine;
FIG. 2 is a schematic view of a scanning apparatus for scanning a plurality of components
of similar design and collecting a first projection while a support platform of the
scanning apparatus is in a first position, in accordance with an embodiment of the
present disclosure;
FIG. 3 is a schematic view of the scanning apparatus of FIG. 2 for collecting a second projection, in accordance with an embodiment of the present
disclosure;
FIG. 4 is a schematic view of the scanning apparatus of FIG. 2 while the support platform is shown in a second position, in accordance with an
embodiment of the present disclosure; and
FIG. 5 is a flowchart of a method for scanning a plurality of components of similar design,
in accordance with an embodiment of the present disclosure.
DETAILED DESCRIPTION
[0031] Aspects and embodiments of the present disclosure will now be discussed with reference
to the accompanying Figures. Further aspects and embodiments will be apparent to those
skilled in the art.
[0032] FIG. 1 shows a schematic sectional side view of a gas turbine engine 10 having a principal
rotational axis X-X'. The gas turbine engine 10 includes, in axial flow series, an
air intake 11, a compressive fan 12 (which may also be referred to as a low-pressure
compressor), an intermediate pressure compressor 13, a high-pressure compressor 14,
a combustion equipment 15, a high-pressure turbine 16, an intermediate pressure turbine
17, a low-pressure turbine 18, and a core exhaust nozzle 19. A nacelle 21 generally
surrounds the gas turbine engine 10 and defines the air intake 11, a bypass duct 22,
and a bypass exhaust nozzle 23.
[0033] The gas turbine engine 10 works in a conventional manner so that the air entering
the air intake 11 is accelerated by the compressive fan 12 to produce two air flows:
a first air flow A into the intermediate pressure compressor 13 and a second air flow
B which passes through the bypass duct 22 to provide a propulsive thrust. The intermediate
pressure compressor 13 compresses the first air flow A directed into it before delivering
that air to the high-pressure compressor 14 where further compression takes place.
[0034] The compressed air exhausted from the high-pressure compressor 14 is directed into
the combustion equipment 15 where it is mixed with fuel and the mixture combusted.
The resulting hot combustion products then expand through, and thereby drive the high,
intermediate, and low-pressure turbines 16, 17, 18 before being exhausted through
the core exhaust nozzle 19 to provide additional propulsive thrust. The high, intermediate,
and low-pressure turbines respectively drive the high and intermediate pressure compressors,
14, 13, and the compressive fan 12 by suitable interconnecting shafts.
[0035] In some embodiments, the gas turbine engine 10 is used in an aircraft. In some embodiments,
the gas turbine engine 10 is an ultra-high bypass ratio engine (UHBPR). In addition,
the present invention is equally applicable to aero gas turbine engines, marine gas
turbine engines and land-based gas turbine engines.
[0036] FIG. 2 is a schematic view of a scanning apparatus 100 for scanning a plurality of components
102 of similar design and collecting a first projection 120, in accordance with an
embodiment of the present disclosure. The scanning apparatus 100 performs a computational
tomography (CT), preferably a three-dimensional CT, of the component. In some embodiments,
the plurality of components 102 is a part of the gas turbine engine 10 (shown in
FIG. 1). In other embodiments, the plurality of components 102 is a part of another prime
mover or a machine. In some embodiments, the plurality of components 102 includes
turbine blades or compressor blades of the gas turbine engine 10 (shown in
FIG. 1). In some embodiments, the plurality of components 102 is metallic. The plurality of
components 102 is shown schematically in
FIG. 2 for the purpose of illustration. Other shapes and designs for the plurality of components
102 are foreseeable and could be used.
[0037] It should be noted that "components of similar design" refers to components that
have similar shape, or components that are axi-symmetric (i.e., symmetrical around
one axis). For examples, components, such as gears will be considered as components
of similar design. By similar design of the plurality of components 102, it may also
mean that an overall shape and dimensions of each component 102 are similar to each
other, neglecting variation in tolerances and machining.
[0038] Further, the scanning apparatus 100 includes an imaging beam source 108 configured
to generate an imaging beam 110 that passes through the plurality of components 102.
In some embodiments, the imaging beam source 108 is an electromagnetic source, such
as an x-ray source or a gamma-ray source. The imaging beam source 108 is capable of
emitting the imaging beam 110 in the electromagnetic spectrum that can penetrate or
be transmitted through a material after attenuation. In some embodiments, the x-ray
source may be one of a reflective x-ray source or a transmissive x-ray source.
[0039] The scanning apparatus 100 further includes an imaging beam receiver 114 configured
to receive the imaging beam 110, such that the plurality of components 102 is disposed
between the imaging beam source 108 and the imaging beam receiver 114. In response
to receiving the imaging beam 110, an image may be generated at the imaging beam receiver
114. The scanning apparatus 100 further includes a support platform 104 configured
to support the plurality of components 102. In other words, the plurality of component
102 is disposed on the support platform 104. Further, the support platform 104 is
configured to rotate and/or revolve relative to the imaging beam source 108 and the
imaging beam receiver 114 about one or more axes. The support platform 104 is disposed
between the imaging beam source 108 and the imaging beam receiver 114.
[0040] As shown in
FIG. 2, the plurality of components 102 is positioned axi-symmetrically and spaced apart
from each other by a first angular range AR1. In the illustrated embodiment of
FIG. 2, six components (depicted by numerals 1, 2, 3, 4, 5, and 6) are shown to be disposed
axi-symmetrically on the support platform 104. In some embodiments, the number of
components may be less than 6 or more than 6. However, it should be noted that the
plurality of components 102 should be arranged axi-symmetrically with each component
102 spaced apart by a predetermined angular range, for example, the first angular
range AR1. In some embodiments, the plurality of components 102 is positioned offset
from the one or more axes of rotation and/or revolution. This may improve image quality
and contrast of the scan. This may also reduce the concave wall effect.
[0041] In the illustrated embodiment of
FIG. 2, the first angular range AR1 is shown as 60 degrees. In other words, the plurality
of components 102 is shown to be spaced apart from each other by 60 degrees. However,
it may vary based on the number of components 102 disposed on the support platform
104 or based on application requirements. In some embodiments, the first angular range
AR1 is at least 5 degrees, at least 10 degrees, at least 20 degrees, at least 30 degrees,
at least 45 degrees, at least 60 degrees, at least 90 degrees, at least 120 degrees,
at least 135 degrees, at least 150 degrees, at least 170 degrees, at least 200 degrees,
at least 230 degrees, or at least 270 degrees.
[0042] In some embodiments, the plurality of components 102 is positioned axi-symmetrically
in a two-dimensional geometrical figure, such as a circle, a triangle, an ellipse,
a rectangle, a square, or a polygon. For example, the plurality of components is positioned
on vertices of a triangle. For example, the plurality of components is positioned
on vertices of a square.
[0043] In some embodiments, the plurality of components 102 is positioned axi-symmetrically
in a three-dimensional geometrical figure, such as an ellipsoid, a sphere, a cube,
a cuboid, a prism, or a cylinder. This arrangement of the plurality of components
102 in the three-dimensional geometrical figure may ensure proper utilization of available
space to accommodate the plurality of components 102 on the support platform 104.
For example, the plurality of components 102 is positioned on corners of a cube.
[0044] In some embodiments, the plurality of components 102 is positioned axi-symmetrically
in two or more concentric geometrical figures. In some embodiments, the two or more
concentric geometrical figures have same shapes. For example, some of the components
102 may be positioned axi-symmetrically in a first circle and rest of the components
102 may be positioned axi-symmetrically in a second circle that is concentric with
the first circle. In other embodiments, the two or more concentric geometrical figures
have different shapes. For example, some of the components 102 may be positioned axi-symmetrically
in a circle and rest of the components 102 may be positioned axi-symmetrically in
a square that is concentric with the circle.
[0045] The scanning apparatus 100 further includes a processor 116 communicably coupled
to the imaging beam receiver 114. The processor 116 further includes a memory 118
configured to store processor-executable instructions, which, on execution, may cause
the processor 116 to perform one or more operations. The processor 116 may be a controller,
a control circuit, a computer, a microprocessor, a microcomputer, a central processing
unit, or any suitable device or apparatus. The processor 116 may be a digital processor,
an analog processor, a digital circuit designed to process information, an analog
circuit designed to process information, a state machine, and/or other mechanisms
for electronically processing information.
[0046] FIG. 3 is a schematic view of the scanning apparatus 100 of
FIG. 2 for collecting a second projection 122, in accordance with an embodiment of the present
disclosure. As shown in
FIG. 3, the scanning apparatus 100 further includes an anti-scatter unit 106. Further, the
anti-scatter unit 106 is selectively disposed either between the support platform
104 and the imaging beam receiver 114, or between the support platform 104 and the
imaging beam source 108. In the illustrated embodiment of
FIG. 3, the anti-scatter unit 106 is disposed between the support platform 104 and the imaging
beam receiver 114.
[0047] In some embodiments, the anti-scatter unit 106 includes an anti-scatter grid, a beam
stopper, a hole plate array, or a collimation grid. The anti-scatter grid is often
used in CT scanning to reduce the scattered radiation generated from an object to
be scanned. The hole plate array may block the imaging beam from deviating from a
primary beam path, thereby capturing scatter free projections at the imaging beam
receiver 114. In the illustrated embodiment of
FIG. 3, the anti-scatter unit 106 includes an anti-scatter grid. Further, in the illustrated
embodiment of
FIG. 2, the anti-scatter unit 106 is not used (and hence not shown in
FIG. 2) for collecting the first projection 120.
[0048] Referring to
FIGS. 2 and 3, the processor 116 is configured to collect, in absence of the anti-scatter unit 106,
the first projection 120 of at least one component 102 of the plurality of components
102 at the imaging beam receiver 114. The first projection 120 includes a combination
of a primary image PI of the at least one component 102 and a scatter image SI of
the at least one component 102. The primary image PI includes a scatter free projection
of the at least one component 102.
[0049] The processor 116 is further configured to collect, in presence of the anti-scatter
unit 106 (shown in
FIG. 3), the second projection 122 of the at least one component 102 at the imaging beam receiver
114. The second projection 122 includes the primary image PI of the at least one component
102. In the present disclosure, the anti-scatter unit 106 is used while collecting
the primary image PI (i.e., scatter free projection) of an object, however, other
techniques may also be used to obtain a scatter free projection of an object subjected
to scanning. In the illustrated embodiment of
FIGS. 2 and 3, the support platform is in a first position P1.
[0050] The processor 116 is further configured to compare the first projection 120 and the
second projection 122. In some embodiments, the processor 116 is configured to compare
the first projection 120 and the second projection 122 by subtracting the second projection
122 from the first projection 120. In other applications, the first projection may
be subtracted from the second projection. Upon comparing the first projection 120
and the second projection 122, the processor 116 is further configured to generate
the scatter image SI based on the comparison of the first projection 120 and the second
projection 122. In some embodiments, the processor 116 is configured to generate the
scatter image SI by subtracting the second projection 122 from the first projection
120. The processor 116 is further configured to store the scatter image SI of the
at least one component 102 in the memory 118.
[0051] The processor 116 is further configured to collect, at different relative angles
of rotation and/or revolution of the support platform 104 and in absence of the anti-scatter
unit 106, further projections of the plurality of components 102 at the imaging beam
receiver 114. The support platform 104 is configured to rotate and/or revolve by a
second angular range AR2 relative to the imaging beam source 108 and the imaging beam
receiver 114 about one or more axes. When the support platform 104 is rotated by the
second angular range AR2, the support platform 104 moves from the first position P1
(shown in
FIG. 2) to another position. In some embodiments, the second angular range AR2 is at least
5 degrees, at least 10 degrees, at least 15 degrees, at least 25 degrees, at least
35 degrees, at least 50 degrees, at least 65 degrees, at least 95 degrees, at least
125 degrees, at least 140 degrees, at least 155 degrees, at least 175 degrees, at
least 200 degrees, at least 230 degrees, at least 270 degrees, or at least 290 degrees.
[0052] FIG. 4 is a schematic view of the scanning apparatus 100, wherein the support platform 104
is shown in a second position P2 which is a result of rotation of the support platform
104 by the second angular range AR2 relative to the first position P1. The second
angular range AR2 is equal to or greater than the first angular range AR1 by at most
20 degrees. In the illustrated embodiment of
FIG. 4, the second angular range AR2 is about 75 degrees.
[0053] It is evident from
FIG. 4, that the all the components 102 (depicted by numerals 1, 2, 3, 4, 5, and 6) are moved
from its previous position to a new position due to rotation of the support platform
104 by the second angular range AR2. However, it should be noted that only the support
platform 104 is rotated by the second angular range AR2, therefore the angle between
different components would not change. In other words, the plurality of adjacent components
102 would remain spaced apart from each other by the first angular range AR1.
[0054] The processor 116 is further configured to compare the further projections and the
scatter image SI. In some embodiments, the processor 116 is further configured to
compare the further projections and the scatter image SI by subtracting the scatter
image SI from each of the further projections. Upon comparing the further projections
and the scatter image SI, the processor 116 is further configured to generate further
primary images of the plurality of components 102. In some embodiments, the processor
116 is configured to generate the further primary images of the plurality of components
102 by subtracting the scatter image SI from each of the corresponding further projections.
The further primary images include corresponding further scatter free projections
of the plurality of components 102
[0055] With axi-symmetric arrangement of the plurality of components 102 of similar design
on the support platform 104, and with each component spaced apart by a predetermined
angular range (i.e., the first angular range AR1), the scanning apparatus 100 may
eliminate a need for a full 360-degrees rotation for collecting projections of various
components 102. This arrangement of the plurality of components 102 may ensure periodic
repetition of the further projections at different relative angles of rotation and/or
revolution of the support platform 104 by the second angular range AR2. Such periodic
repetition of the further projections may enable the scanning apparatus 100 to perform
scatter correction only once. This may significantly reduce scanning time and computational
efforts required to generate the reference scatter image SI, which was otherwise needed
to be generated for each projection in conventional scanning techniques. Therefore,
the scanning apparatus 100 may improve efficiency and accuracy of the scanning process
for investigating the plurality of components 102 of similar design. Accordingly,
the scanning apparatus 100 may enable the simultaneous and effective scanning of the
plurality of components 102, which may further reduce operational cost involved with
the scanning.
[0056] FIG. 5 is a flowchart of a method 200 for scanning the plurality of components 102 shown
in
FIGS. 2 to 4, according to an embodiment of the present disclosure. The method 200 may be at least
partly performed by the scanning apparatus 100 of
FIGS. 2 to 4. Referring to
FIGS. 2 to 5, at step 202, the method 200 includes providing the imaging beam source 108, the imaging
beam receiver 114, and the support platform 104. The imaging beam source 108 and the
imaging beam receiver 114 are oppositely disposed to either side of the support platform
104.
[0057] At step 204, the method 200 further includes disposing the plurality of components
102 on the support platform 104 such that the plurality of components 102 is positioned
axi-symmetrically and spaced apart from each other by the first angular range AR1.
[0058] At step 206, the method 200 further includes generating, by the imaging beam source
108, the imaging beam 110 that passes through the plurality of components 102. At
step 208, the method 200 further includes collecting the first projection 120 of at
least one component 102 of the plurality of components 102 at the imaging beam receiver
114.
[0059] At step 210, the method 200 further includes collecting the second projection 122
of the at least one component 102 at the imaging beam receiver 114. In some embodiments,
for collecting the second projection 122, the method 200 further includes selectively
disposing the anti-scatter unit 106 either between the support platform 104 and the
imaging beam receiver 114, or between the support platform 104 and the imaging beam
source 108. In some embodiments, collecting the second projection 122 of the at least
one component 102 at the imaging beam receiver 114 further includes collecting the
second projection 122 of the at least one component 102 at the imaging beam receiver
114, while the anti-scatter unit 106 is disposed between the support platform 104
and the imaging beam receiver 114, or between the support platform 104 and the imaging
beam source 108.
[0060] At step 212, the method 200 further includes comparing, by the processor 116, the
first projection 120 and the second projection 122. In some embodiments, comparing
the first projection 120 and the second projection 122 includes subtracting the second
projection 122 from the first projection 120.
[0061] At step 214, the method 200 further includes generating, by the processor 116, the
scatter image SI based on the comparison of the first projection 120 and the second
projection 122. In some embodiments, the method 200 includes generating the scatter
image SI based on subtraction of the second projection 122 from the first projection
120. By subtracting the second projection 122 from the first projection 120, a reference
scatter image is generated, which may be used for scatter correction.
[0062] At step 216, the method 200 further includes storing, by the processor 116, the scatter
image SI of the at least one component 102 in the memory 118. At step 218, the method
200 further includes rotating and/or revolving the support platform 104 by the second
angular range AR2 relative to the imaging beam source 108 and the imaging beam receiver
114 about one or more axes. The second angular range AR2 is equal to the first angular
range AR1 or greater than the first angular range AR1 by at most 20 degrees.
[0063] At step 220, the method 200 further includes collecting, at different relative angles
of rotation and/or revolution of the support platform 104 by the second angular range
AR2, further projections of the plurality of components 102 at the imaging beam receiver
114. In some embodiments, the method 200 further includes maintaining substantially
similar imaging parameters while collecting the further projections.
[0064] At step 222, the method 200 further includes comparing, by the processor 116, the
further projections and the scatter image SI. In some embodiments, comparing the further
projections and the scatter image SI includes subtracting the scatter image SI from
each of the further projections. In some embodiments, the method 200 includes generating
the further primary images of the plurality of components 102 based on subtraction
of the scatter image SI from each of the corresponding further projections.
[0065] At step 224, the method 200 further includes generating, by the processor 116, further
primary images of the plurality of components 102 based on the comparison of the further
projections and the scatter image SI, the further primary images include corresponding
further scatter free projections of the plurality of components 102. The reference
scatter image is then subtracted from the further projections of the plurality of
components 102. Accordingly, a high-quality primary image is obtained while minimizing
an impact of scatter.
[0066] Various examples have been described, each of which comprise one or more combinations
of features. It will be appreciated by those skilled in the art that, except where
clearly mutually exclusive, any of the features may be employed separately or in combination
with any other features and the invention extends to and includes all combinations
and sub-combinations of one or more features described herein.
1. A method (200) for scanning a plurality of components (102) of similar design, the
method (200) comprising:
providing an imaging beam source (108), an imaging beam receiver (114), and a support
platform (104), wherein the imaging beam source (108) and the imaging beam receiver
(114) are oppositely disposed to either side of the support platform (104);
disposing the plurality of components (102) on the support platform (104) such that
the plurality of components (102) is positioned axi-symmetrically and spaced apart
from each other by a first angular range (AR1);
generating, by the imaging beam source (108), an imaging beam (110) that passes through
the plurality of components (102);
collecting a first projection (120) of at least one component (102) of the plurality
of components (102) at the imaging beam receiver (114), the first projection (120)
comprising a combination of a primary image (PI) of the at least one component (102)
and a scatter image (SI) of the at least one component (102), wherein the primary
image (PI) comprises a scatter free projection of the at least one component (102);
collecting a second projection (122) of the at least one component (102) at the imaging
beam receiver (114), the second projection (122) comprising the primary image (PI)
of the at least one component (102);
comparing, by a processor (116), the first projection (120) and the second projection
(122);
generating, by the processor (116), the scatter image (SI) based on the comparison
of the first projection (120) and the second projection (122);
storing, by the processor (116), the scatter image (SI) of the at least one component
(102) in a memory (118);
rotating and/or revolving the support platform (104) by a second angular range (AR2)
relative to the imaging beam source (108) and the imaging beam receiver (114) about
one or more axes, wherein the second angular range (AR2) is equal or greater than
the first angular range (AR1) by at most 20 degrees;
collecting, at different relative angles of rotation and/or revolution of the support
platform (104) by the second angular range (AR2), further projections of the plurality
of components (102) at the imaging beam receiver (114);
comparing, by the processor (116), the further projections and the scatter image (SI);
and
generating, by the processor (116), further primary images of the plurality of components
(102) based on the comparison of the further projections and the scatter image (SI),
the further primary images comprising corresponding further scatter free projections
of the plurality of components (102).
2. The method (200) of claim 1, wherein comparing the first projection (120) and the
second projection (122) comprises subtracting the second projection (122) from the
first projection (120), and wherein the method (200) comprises generating the scatter
image (SI) based on subtraction of the second projection (122) from the first projection
(120).
3. The method (200) of claim 1 or claim 2, wherein comparing the further projections
and the scatter image (SI) comprises subtracting the scatter image (SI) from each
of the further projections, and wherein the method (200) comprises generating the
further primary images of the plurality of components (102) based on subtraction of
the scatter image (SI) from each of the corresponding further projections.
4. The method (200) of any one of claims 1 to 3, wherein the first angular range (AR1)
is at least 5 degrees, at least 10 degrees, at least 20 degrees, at least 30 degrees,
at least 45 degrees, at least 60 degrees, at least 90 degrees, at least 120 degrees,
at least 135 degrees, at least 150 degrees, at least 170 degrees, at least 200 degrees,
at least 230 degrees, or at least 270 degrees.
5. The method (200) of any one of claims 1 to 4, wherein the second angular range (AR2)
is at least 5 degrees, at least 10 degrees, at least 15 degrees, at least 25 degrees,
at least 35 degrees, at least 50 degrees, at least 65 degrees, at least 95 degrees,
at least 125 degrees, at least 140 degrees, at least 155 degrees, at least 175 degrees,
at least 200 degrees, at least 230 degrees, at least 270 degrees, or at least 290
degrees.
6. The method (200) of any one of claims 1 to 5, wherein the plurality of components
(102) is positioned axi-symmetrically in a two-dimensional geometrical figure, such
as a circle, a triangle, an ellipse, a rectangle, a square, or a polygon.
7. The method (200) of any one of claims 1 to 5, wherein the plurality of components
(102) is positioned axi-symmetrically in a three-dimensional geometrical figure, such
as an ellipsoid, a sphere, a cube, a cuboid, a prism, or a cylinder.
8. The method (200) of any one of claims 1 to 5, wherein the plurality of components
(102) is positioned axi-symmetrically in two or more concentric geometrical figures.
9. The method (200) of any one of claims 1 to 8, further comprising maintaining substantially
similar imaging parameters while collecting the further projections.
10. The method (200) of any one of claims 1 to 9, further comprising selectively disposing
an anti-scatter unit (106) either between the support platform (104) and the imaging
beam receiver (114) or between the support platform (104) and the imaging beam source
(108).
11. The method (200) of claim 10, wherein collecting the second projection (122) of the
at least one component (102) at the imaging beam receiver (114) further comprises
collecting the second projection (122) of the at least one component (102) at the
imaging beam receiver (114) while the anti-scatter unit (106) is disposed between
the support platform (104) and the imaging beam receiver (114), or between the support
platform (104) and the imaging beam source (108).
12. A scanning apparatus (100) for scanning a plurality of components (102) of similar
design, the scanning apparatus (100) comprising:
an imaging beam source (108) configured to generate an imaging beam (110) that passes
through the plurality of components (102);
an imaging beam receiver (114) configured to receive the imaging beam (110), such
that the plurality of components (102) is disposed between the imaging beam source
(108) and the imaging beam receiver (114);
an anti-scatter unit (106);
a support platform (104) configured to support the plurality of components (102),
wherein the support platform (104) is configured to rotate and/or revolve relative
to the imaging beam source (108) and the imaging beam receiver (114) about one or
more axes, wherein the support platform (104) is disposed between the imaging beam
source (108) and the imaging beam receiver (114), wherein the plurality of components
(102) is positioned axi-symmetrically and spaced apart from each other by a first
angular range (AR1); and
a processor (116) communicably coupled to the imaging beam receiver (114) and configured
to:
collect, in absence of the anti-scatter unit (106), a first projection (120) of at
least one component (102) of the plurality of components (102) at the imaging beam
receiver (114), the first projection (120) comprising a combination of a primary image
(PI) of the at least one component (102) and a scatter image (SI) of the at least
one component (102), wherein the primary image (PI) comprises a scatter free projection
of the at least one component (102);
collect, in presence of the anti-scatter unit (106), a second projection (122) of
the at least one component (102) at the imaging beam receiver (114), the second projection
(122) comprising the primary image (PI) of the at least one component (102);
compare the first projection (120) and the second projection (122);
generate the scatter image (SI) based on the comparison of the first projection (120)
and the second projection (122);
store the scatter image (SI) of the at least one component (102) in a memory (118);
collect, at different relative angles of rotation and/or revolution of the support
platform (104) and in absence of the anti-scatter unit (106), further projections
of the plurality of components (102) at the imaging beam receiver (114), wherein the
support platform (104) is configured to rotate and/or revolve by a second angular
range (AR2) relative to the imaging beam source (108) and the imaging beam receiver
(114) about one or more axes, wherein the second angular range (AR2) is equal to or
greater than the first angular range (AR1) by at most 20 degrees;
compare the further projections and the scatter image (SI); and
generate further primary images (PI) of the plurality of components (102) based on
the comparison of the further projections and the scatter image (SI), the further
primary images comprising corresponding further scatter free projections of the plurality
of components (102).
13. The scanning apparatus (100) of claim 12, wherein the processor (116) is further configured
to:
compare the first projection (120) and the second projection (122) by subtracting
the second projection (122) from the first projection (120); and
generate the scatter image (SI) by subtracting the second projection (122) from the
first projection (120).
14. The scanning apparatus (100) of claim 12 or claim 13, wherein the processor (116)
is further configured to:
compare the further projections and the scatter image (SI) by subtracting the scatter
image (SI) from each of the further projections; and
generate the further primary images of the plurality of components (102) by subtracting
the scatter image (SI) from each of the corresponding further projections.
15. The scanning apparatus (100) of any one of claims 12 to 14, wherein the anti-scatter
unit (106) is selectively disposed either between the support platform (104) and the
imaging beam receiver (114), or between the support platform (104) and the imaging
beam source (114).